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Hydrant Valve and Coupler Historical Background

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • AIR4782B
  • Current
Published 2018-01-03 by SAE International in United States
This SAE Aerospace Information Report (AIR) presents historical information and background data related to hydrant valves and couplers used in worldwide ground refueling of commercial aircraft (hereafter generically referred to as hydrant devices). Military hydrant devices are not included since their mission requirements demand approaches that may differ.
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Detailed Specification for Aircraft Pressure Refueling Nozzle

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • AS5877B
  • Current
Published 2016-11-29 by SAE International in United States
This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling and defueling of aircraft fitted with pressure fuel servicing systems. It is to be used as a replacement for MIL-N-5877, MS29520 and for all commercial applications.
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Aircraft Refueling Vehicle Design and Performance Requirements

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • ARP5818A
  • Current
Published 2015-08-13 by SAE International in United States
This document is a guideline for the design and operation of Aviation Aircraft Refueling Vehicles and for the materials, components, and systems used thereon. The criteria set forth herein are the minimum recommendations for all types of aircraft refueling vehicles, including tanker vehicles, hydrant service vehicles, towable hydrant carts, fixed refueling cabinets, and any other type of aircraft refueling vehicles used at airports for aircraft refueling operations with nominal operating fuel pressures and flow rates as specified within this document.
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Standard Test Procedure and Limit Value for Shutoff Surge Pressure of Pressure Fuel Dispensing Systems

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • AS1284B
  • Current
Published 2015-07-17 by SAE International in United States
The test procedure and related limit value are intended to apply to fixed and mobile ground pressure fuel dispensing systems and to aerial refueling tankers.
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Design and Operation of Aircraft Refueling Tanker Vehicles

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • ARP5818
  • Historical
Published 2011-11-16 by SAE International in United States
This document is a guideline for the design of an Aviation Aircraft Refueling and Defueling Tanker Vehicle and for the materials and components used thereon. The criteria set forth herein are the minimum recommendations and are limited to aircraft refueling vehicles for airport operations with operating fuel pressures and flow rates as specified within this document.
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Aircraft Fueling Adapter Wear Limits

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • ARP5298
  • Current
Published 2011-11-16 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) defines the wear limits allowed on certain features of Pressure Fuel Servicing Adapters which are crucial for safe interfacing of Pressure Fuel Servicing Nozzles and Pressure Caps. Wear limits as described herein represent the maximum amount of wear on certain features of the Adapter beyond which use of the Adapter for these purposes may contribute to an unsafe condition. Such wear is the result of the normal use of the Adapter for aircraft refueling and also, in some cases, for Nozzle stowage on refueling vehicles.
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Aviation Fuel Facilities

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • ARP5789
  • Current
Published 2011-11-16 by SAE International in United States
This document contains general criteria for the planning, design, and construction of military and commercial ground based aviation fueling facilities that receive, store, distribute, and dispense liquid aviation turbine fuels at airports to both fixed and rotary wing aircraft.
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Standard Test Criteria for Aircraft Refuelers

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • ARP5918
  • Current
Published 2011-11-16 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) establishes the minimum recommended Test Stand Setup and Procedures for inspecting and testing Aircraft Refuelers. The inspection and test procedure shall be used to evaluate the operation and performance of an Aircraft Refueler to assure that it meets the minimum refueling performance criteria and is fit for aircraft fueling and/or defueling operations. These procedures shall be used to test new Aircraft Refuelers and may be used to perform routine tests to confirm that the Aircraft Refuelers comply with the minimum performance criteria as specified herein. This document covers all types of Aircraft Refuelers, stationary (e.g., cabinet type units) or mobile (e.g., hydrant service vehicles, tankers, etc). NOTE: Aircraft refueling vehicle design and operating requirements are provided in separate SAE ARP Documents. NOTE: This document does NOT address Aircraft Refuelers with operating pressure above 150 psi although many of the paragraphs can be used as a guideline.
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STANDARD TEST PROCEDURE AND LIMIT VALUE FOR SHUTOFF SURGE PRESSURE OF PRESSURE FUEL DISPENSING SYSTEMS

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • AS1284
  • Historical
Published 2011-08-15 by SAE International in United States
The test procedure and related limit value are intended to apply to all ground pressure fuel dispensing systems, fixed and mobile.
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Hydrant Valve and Coupler Historical Background

AE-5C Aviation Ground Fueling Systems Committee
  • Aerospace Standard
  • AIR4782A
  • Historical
Published 2008-08-12 by SAE International in United States
This SAE Aerospace Information Report (AIR) presents historical information and background data related to hydrant valves and couplers used in worldwide ground refueling of commercial aircraft (hereafter generically referred to as hydrant devices). Military hydrant devices are not included since their mission requirements demand approaches that may differ.
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